• 제목/요약/키워드: Turbine rotor

검색결과 882건 처리시간 0.027초

75톤급 액체로켓엔진 터보펌프용 속도복식 터빈개발 (Development of a Velocity Compounded Impulse Turbine for the 75ton Liquid Rocket Engine Application)

  • 정은환;이항기;박편구;김진한
    • 한국추진공학회지
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    • 제15권3호
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    • pp.40-46
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    • 2011
  • 75톤급 터보펌프용 속도복식 터빈을 개발하였다. 축과 로터의 연결에는 커빅커플링을 적용하였다. 커빅커플링은 시편을 통한 고온비틀림 시험과 시제품의 스핀시험을 통해 적용 적합성을 검증하였다. 고압 공기를 이용한 성능시험 결과, 개량형 속도복식 터빈의 비출력은 기본형 단단 터빈에 비해 설계점에서 20.5%가량 향상된 것으로 나타났다. 개량형터빈의 $1^{st}$로터는 설계점 전체출력의 74.1%를 담당하는 것으로 확인되었다.

상용 유한요소 해석 프로그램을 이용한 가스터빈 간극 설계의 가시화 방법 (Visualization method of Clearance Design of Gas Turbine using Commercial Finite Element Analysis program)

  • 한도원;김영춘;김경천
    • 한국가시화정보학회지
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    • 제17권1호
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    • pp.78-84
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    • 2019
  • A gas turbine is the main equipment of a power plant that generates electricity by high-speed rotation of the rotor in a high-temperature environment. In particular, in the case of medium to large-sized gas turbines, the rotor is composed of a plurality of stages, and each component is exposed to different physical environments. Especially, in the case of the tip clearance of the turbine, it is a very important factor in the performance of the design items and the operation of the stable turbine, and a design considering the physical behavior of all major parts should be done. In this study, we will discuss the process of visualizing the physical behavior of turbine operating conditions and the method of designing tip clearance for stable operation by using commercial finite element analysis program for gas turbine assembly model and single product.

고속회전체 밸런싱 시험기 개발 (Development of High Speed Rotor Balancing Machine)

  • 이영섭;이정훈;김창근;김명섭
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.1078-1083
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    • 2000
  • A high speed rotor balancing machine was developed, which is capable of balancing a flexible rotor in high speed. The machine is largely consisted of vacuum chamber, oil supply system and vacuum pump system. And, in order to investigate performances of the machine, various tests were carried. After high speed rotor balancing of gas turbine engine rotor using influence coefficient method, the flexible engine rotor passed smoothly through its critical speed.

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터보펌프용 1.4MW급 터빈의 전산유동해석

  • 박편구;정은환;김진한
    • 항공우주기술
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    • 제4권2호
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    • pp.153-162
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    • 2005
  • 초기 설계과정에서 4가지 1.4MW급 터보펌프용 터빈설계안을 도출한 후 각각의 설계안에 대하여 프로즌 로터기법을 적용한 3차원 유동해석을 수행하였다. 이 결과를 통하여 각각의 설계안간의 성능을 비교하고 가장 성능이 우수한 설계안을 선정하였다. 계산결과의 분석을 통하여 유로에서의 유동특성과 충격파와 후류에 의해 발생되는 손실을 파악하였으며 이 분석 결과를 바탕으로 보다 우수한 성능을 보일 것으로 예측되는 설계안을 도출한 후 이에 대한 3차원 유동해석을 수행하여 결과를 분석하였다.

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Numerical Prediction of Unsteady Flows through Whole Nozzle-Rotor Cascade Channels with Partial Admission

  • Sasao, Yasuhiro;Monma, Kazuhiro;Tanuma, Tadashi;Yamamoto, Satoru
    • International Journal of Fluid Machinery and Systems
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    • 제2권3호
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    • pp.248-253
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    • 2009
  • This paper presents a numerical study for unsteady flows in a high-pressure steam turbine with a partial admission stage. Compressible Navier-Stokes equations are solved by the high-order high-resolution finite-difference method based on the fourth-order compact MUSCL TVD scheme, Roe's approximate Riemann solver, and the LU-SGS scheme. The SST-model is also solved for evaluating the eddy-viscosity. The unsteady two-dimensional flows through whole nozzle-rotor cascade channels considering a partial admission are numerically investigated. 108 nozzle passages with two blockages and 60 rotor passages are simultaneously calculated. The influence of the flange in the nozzle box to the lift of rotors is predicted. Also the efficiency of the partial admission stage changing the number of blockages and the number of nozzles is parametrically predicted.

750kW 로터 블레이드 인증시험 (Proof Test of a 750kW Wind Turbine Blade)

  • 김명진;성대영;박병준
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2008년도 추계학술대회 논문집
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    • pp.328-331
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    • 2008
  • For the purpose of verifying the calculation, the rotor blade shall be subjected to test for the natural frequencies and the static loading within the scope of the assessment. This paper presents a full scale static test procedure of the rotor blade for certification by GL. This blade model is manes as KM24 designed for IEC type IA. The test and calculation values are all most similar. Also there is not founded any marks of cracks or buckling at the shell, and bonding area is T/E, L/E and shear web. Therefore, the test is successful and the rotor blade is satisfied the safety requirement at the maximum design load.

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터빈발전기의 축계 진동 해석: 열박음형과 용접형 로터의 진동 특성 비교 (Vibration Analysis of Rotating System in a Turbine and Generator Set: Comparison of Shrunk-fit Disc Rotor and Welded Drum Rotor)

  • 하현천;박철현;최성필;김계연
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 추계학술대회논문집
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    • pp.599-604
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    • 2000
  • Excessive vibration magnitude results in serious damage and economic losses in the turbine and generator system. Therefore, it is of importance to evaluate the accurate dynamic characteristics of the system in advance. In this paper, rotordynamic characteristics of both the shrunk-fit disc and welded drum rotors have been investigated to ensure an excellent running behavior of the system in which low-pressure(LP) turbines of a nuclear power plant were retrofitted to improve thermal efficiency and reliability. Analysis shows that the welded drum rotor has good torsional characteristics rather than the shrunk-fit disc rotor. In addition, verification testing of field test was performed to confirm the retrofit. Test results are good agreement with analysis ones.

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로터 블레이드 결빙에 의한 타워 피로하중 평가 (Evalulation of the Tower Fatigue Loads by Ice Formation on Rotor Blades)

  • 김정기;박선호;방조혁;정종훈;김상덕;류지윤
    • 풍력에너지저널
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    • 제5권1호
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    • pp.43-49
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    • 2014
  • Primarily, tower loads of a wind turbine arise from aerodynamic effect and a top head mass. But sometime asymmetric loads of rotor also affect on the tower loads. Especially ice formation on two blades out of three causes the asymmetric loads, because the ice formation on blades lead to large rotating mass imbalance. This rotating mass imbalance of rotor affects tower fatigue loads. So design load cases of ice formation on blade should be considered in the fatigue design loads of the tower according to GL guideline 2010. This paper describes the change of tower fatigue loads following increase of tower height in the condition of ice formation. Finally, the optimal operation strategy is examined in order to reduce tower fatigue design loads.

동특성해석을 위한 계통연계 풍력발전 시스템의 모델링 (Modeling of a Grid-Connected Wind Energy Conversion System for Dynamic Performance Analysis)

  • 추연식;노경수
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2002년도 하계학술대회 논문집 B
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    • pp.1358-1360
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    • 2002
  • This paper presents a modeling and simulation of a utility-connected wind energy conversion system with a link of a rectifier and an inverter. It discusses the maximum power control algorithm for the wind turbine and presents the relationship of wind turbine output, rotor speed, power coefficient, tip-speed ratio and wind speed when the wind turbine is operated under the maximum power control algorithm. The control objective is to extract maximum power from wind and transfer the power to the utility. This is achieved by controlling the pitch angle of the wind turbine blades. Pitch control method is mechanically complicated, but the control performance is better than that of the stall regulation method. The simulation results performed on MATLAB will show the variation of generator's rotor speed, pitch angle, and generator output.

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개별 블레이드 피치 제어 방식을 이용한 수직축 풍력발전기의 성능 해석 및 시스템 구현 (Aerodynamic Analysis and System Implementation of Vertical Axis Wind Turbine using Individual Blade Pitch Control Method)

  • 정인오;이윤한;황인성;김승조
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.3347-3352
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    • 2007
  • This paper describes a research for the performance improvement of the straight-bladed vertical axis wind turbine. To improve the performance of VAWT, the individual blade pitch control method is adopted. For the wind turbine, CFD analysis is carried out by changing blade pitch angle according to the change of wind speed and wind direction. By this method, capacity and power efficiency of VAWT are obtained according to the wind speed and rotating of rotor, and could predict the overall performance of VAWT. It was manufactured to verify performance of the experimental system that consists of rotor including four blades and base. Furthermore, torque sensor and power generator were installed. Also, active controller which can change the pitch angle of the individual blade according to the wind speed and direction was used.

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